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Adhesive Bonding of End Closures for High Strength and Reliability in in Rocket Motor Cases

机译:火箭发动机壳体高强度和可靠性的端盖粘接

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摘要

Preliminary studies of bonded joint fabrication technique were conducted with 26 uniaxial lap and scarf joint specimens and 17 sub-scale test cases' of 5" nominal diameter and. 18" length. Fifteen of the sub-scale units ex¬ceeded the target bonded joint strength of 3750 psi by an average of 40%. The information gained from these preliminary tests was applied to the fabrication of 16 prototype bonded end closure cases of 16" nominal diameter and 41" length.

著录项

  • 作者

  • 作者单位
  • 年度 1963
  • 页码 1-70
  • 总页数 70
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类 工业技术;
  • 关键词

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